AVUM DEB (ADAPTOR)
Satellite information AVUM DEB (ADAPTOR) - AVUM DEB [ADAPTOR]
| Spacetrack Directory Name | AVUM DEB (ADAPTOR) |
| Alternative name | AVUM DEB [ADAPTOR] |
| Follow AVUM DEB (ADAPTOR) | AVUM DEB (ADAPTOR) Tracker |
| Pass predictions AVUM DEB (ADAPTOR) | Pass predictions AVUM DEB (ADAPTOR) |
| Orbit launches |
2013-05-07 (13 years ago)
|
| Days in orbit | 4860 |
| Country/organisation of origin | European Space Agency (ESA) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 664 km |
| Apogee | 799 km |
| Orbit slope (inclination) | 98.81° |
| Laps per day | 15 |
| Height AVUM DEB (ADAPTOR) | 712.76 km |
Additional information AVUM DEB (ADAPTOR)
AVUM DEB (ADAPTOR), 39162 is space debris in SSO originally from a launch on Tue, 07 May 2013 UTC launched from the French Guiana (FRGUI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite AVUM DEB (ADAPTOR) Date of exalting 07.05.2013y. Average height of ISS AVUM DEB (ADAPTOR) hundred 712.76 km. Average velocity AVUM DEB (ADAPTOR) is 27002.99 km/h. Inclination AVUM DEB (ADAPTOR) satellite 98.81°.TLE
Average velocity AVUM DEB (ADAPTOR)
Average inclination AVUM DEB (ADAPTOR)
Mean right ascension of the ascending node (RAAN) AVUM DEB (ADAPTOR)
Mean argument of perigee AVUM DEB (ADAPTOR)
Mean semi-major axis of the orbit AVUM DEB (ADAPTOR)
Mean orbital eccentricity AVUM DEB (ADAPTOR)
ISS
Buy us a coffee!
